A propulsion assembly with a primary duct and a secondary duct, an outer fairing delimiting an outer compartment with an inlet opening, an inner fairing delimiting an inner compartment with an air exhaust aperture, a suction system having an inlet, an outlet and mobile elements that draw the air in via the inlet and deliver the air via the outlet, a drive that drives the mobile elements, a transfer pipe connected to the outlet, a distribution pipe disposed in the inner compartment, connected to the transfer pipe and having nozzles, a supply pipe that opens into the outer compartment and is connected to the inlet, and a regulator that regulates the flow rate of air in the suction system. The outside air is then driven by the suction system and passes through the two compartments in a forced manner.


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    Titel :

    ENSEMBLE PROPULSIF POUR AERONEF COMPORTANT UN SYSTEME DE VENTILATION


    Weitere Titelangaben:

    PROPULSION ASSEMBLY FOR AIRCRAFT COMPRISING A VENTILATION SYSTEM
    ANTRIEBSEINHEIT FÜR LUFTFAHRZEUG, DIE EIN BELÜFTUNGSSYSTEM UMFASST


    Beteiligte:
    SOMMERER YANNICK (Autor:in) / ZEBIAN MAXIME (Autor:in)

    Erscheinungsdatum :

    23.11.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Französisch


    Klassifikation :

    IPC:    F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES



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